1989
DOI: 10.2514/3.20504
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Application of output feedback to variable structure systems

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Cited by 90 publications
(39 citation statements)
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“…The key design choice is the selection of an appropriate gain G in (5). A common design methodology (Heck and Ferri 1989, El-Khazali and DeCarlo 1992, Heck et al 1995, Bag et al 1997) is based on synthesizing a static output feedback gain numerically to ensure the so-called reachability condition is satisfied.…”
Section: Control Law Developmentmentioning
confidence: 99%
“…The key design choice is the selection of an appropriate gain G in (5). A common design methodology (Heck and Ferri 1989, El-Khazali and DeCarlo 1992, Heck et al 1995, Bag et al 1997) is based on synthesizing a static output feedback gain numerically to ensure the so-called reachability condition is satisfied.…”
Section: Control Law Developmentmentioning
confidence: 99%
“…Since generating estimates of unavailable internal states is a complex problem on its own, a different kind of SMC, called output feedback SMC, has been proposed in the 1990s. This method requires only output information, restricting the definition of the sliding surface to the states that are available through measured outputs [18][19][20].…”
Section: Introductionmentioning
confidence: 99%
“…In this section we consider controlling the vertical velocity of a specific VTOL aircraft (helicopter) (13) . The linearized model of the VTOL aircraft at the airspeed of 135 knots has the form as (1), the coefficients are The state variable x 1 denotes the horizontal velocity (knots), x 2 denotes the vertical velocity (knots), x 3 represents the pitch rate (degree/sec), and x 4 is the pitch angle (degree).…”
Section: Applicationmentioning
confidence: 99%